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RU2402462C2 - Двигательная установка для летательного аппарата и летательный аппарат, содержащий по меньшей мере одну такую двигательную установку - Google Patents

Двигательная установка для летательного аппарата и летательный аппарат, содержащий по меньшей мере одну такую двигательную установку Download PDF

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Publication number
RU2402462C2
RU2402462C2 RU2008107594/11A RU2008107594A RU2402462C2 RU 2402462 C2 RU2402462 C2 RU 2402462C2 RU 2008107594/11 A RU2008107594/11 A RU 2008107594/11A RU 2008107594 A RU2008107594 A RU 2008107594A RU 2402462 C2 RU2402462 C2 RU 2402462C2
Authority
RU
Russia
Prior art keywords
heat exchanger
turbojet engine
flow
housing
hot air
Prior art date
Application number
RU2008107594/11A
Other languages
English (en)
Russian (ru)
Other versions
RU2008107594A (ru
Inventor
Жан-Марк МАРТИНУ (FR)
Жан-Марк МАРТИНУ
Эрве МАРШЕ (FR)
Эрве МАРШЕ
Original Assignee
Эрбюс Франс
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Эрбюс Франс filed Critical Эрбюс Франс
Publication of RU2008107594A publication Critical patent/RU2008107594A/ru
Application granted granted Critical
Publication of RU2402462C2 publication Critical patent/RU2402462C2/ru

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/115—Heating the by-pass flow by means of indirect heat exchange
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/12—Two-dimensional rectangular
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/22—Three-dimensional parallelepipedal
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/208—Heat transfer, e.g. cooling using heat pipes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • General Health & Medical Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)
RU2008107594/11A 2005-07-28 2006-07-07 Двигательная установка для летательного аппарата и летательный аппарат, содержащий по меньшей мере одну такую двигательную установку RU2402462C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0552352A FR2889250B1 (fr) 2005-07-28 2005-07-28 Ensemble propulseur pour aeronef et aeronef comportant au moins un tel ensemble propulseur
FR0552352 2005-07-28

Publications (2)

Publication Number Publication Date
RU2008107594A RU2008107594A (ru) 2009-09-10
RU2402462C2 true RU2402462C2 (ru) 2010-10-27

Family

ID=36177939

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2008107594/11A RU2402462C2 (ru) 2005-07-28 2006-07-07 Двигательная установка для летательного аппарата и летательный аппарат, содержащий по меньшей мере одну такую двигательную установку

Country Status (9)

Country Link
US (1) US8522529B2 (fr)
EP (1) EP1907281B1 (fr)
JP (1) JP4887364B2 (fr)
CN (1) CN101228069B (fr)
BR (1) BRPI0614447A2 (fr)
CA (1) CA2615273C (fr)
FR (1) FR2889250B1 (fr)
RU (1) RU2402462C2 (fr)
WO (1) WO2007012722A1 (fr)

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FR2889298B1 (fr) * 2005-07-28 2010-11-26 Airbus France Echangeur thermique, ensemble propulseur, et aeronef comportant un tel ensemble propulseur
WO2014159311A1 (fr) 2013-03-14 2014-10-02 United Technologies Corporation Système de ventilation utilisant des tringleries d'inverseur de poussée
GB201310810D0 (en) * 2013-06-18 2013-07-31 Rolls Royce Deutschland & Co Kg An accessory mounting for a gas turbine engine
JP6450076B2 (ja) * 2014-02-24 2019-01-09 三菱航空機株式会社 航空機、航空機のエンジンパイロン、および航空機の機体へのエンジン取付方法
US11808210B2 (en) 2015-02-12 2023-11-07 Rtx Corporation Intercooled cooling air with heat exchanger packaging
US10371055B2 (en) 2015-02-12 2019-08-06 United Technologies Corporation Intercooled cooling air using cooling compressor as starter
US10731560B2 (en) 2015-02-12 2020-08-04 Raytheon Technologies Corporation Intercooled cooling air
US10830148B2 (en) 2015-04-24 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air with dual pass heat exchanger
US10221862B2 (en) 2015-04-24 2019-03-05 United Technologies Corporation Intercooled cooling air tapped from plural locations
US10480419B2 (en) 2015-04-24 2019-11-19 United Technologies Corporation Intercooled cooling air with plural heat exchangers
US10100739B2 (en) 2015-05-18 2018-10-16 United Technologies Corporation Cooled cooling air system for a gas turbine engine
US10794288B2 (en) 2015-07-07 2020-10-06 Raytheon Technologies Corporation Cooled cooling air system for a turbofan engine
US10253695B2 (en) * 2015-08-14 2019-04-09 United Technologies Corporation Heat exchanger for cooled cooling air with adjustable damper
US10287982B2 (en) * 2015-08-14 2019-05-14 United Technologies Corporation Folded heat exchanger for cooled cooling air
US10443508B2 (en) 2015-12-14 2019-10-15 United Technologies Corporation Intercooled cooling air with auxiliary compressor control
EP3478581B1 (fr) 2016-06-30 2021-04-28 Bombardier Inc. Ensemble et procédé de conditionnement d'air chauffé par moteur à bord d'un aéronef
US10669940B2 (en) 2016-09-19 2020-06-02 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and turbine drive
US10794290B2 (en) 2016-11-08 2020-10-06 Raytheon Technologies Corporation Intercooled cooled cooling integrated air cycle machine
US10550768B2 (en) 2016-11-08 2020-02-04 United Technologies Corporation Intercooled cooled cooling integrated air cycle machine
US20180162537A1 (en) 2016-12-09 2018-06-14 United Technologies Corporation Environmental control system air circuit
US10961911B2 (en) 2017-01-17 2021-03-30 Raytheon Technologies Corporation Injection cooled cooling air system for a gas turbine engine
US10995673B2 (en) 2017-01-19 2021-05-04 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox
US10577964B2 (en) 2017-03-31 2020-03-03 United Technologies Corporation Cooled cooling air for blade air seal through outer chamber
US10711640B2 (en) 2017-04-11 2020-07-14 Raytheon Technologies Corporation Cooled cooling air to blade outer air seal passing through a static vane
US10738703B2 (en) 2018-03-22 2020-08-11 Raytheon Technologies Corporation Intercooled cooling air with combined features
US10830145B2 (en) 2018-04-19 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air fleet management system
US10808619B2 (en) 2018-04-19 2020-10-20 Raytheon Technologies Corporation Intercooled cooling air with advanced cooling system
US10718233B2 (en) 2018-06-19 2020-07-21 Raytheon Technologies Corporation Intercooled cooling air with low temperature bearing compartment air
US11255268B2 (en) 2018-07-31 2022-02-22 Raytheon Technologies Corporation Intercooled cooling air with selective pressure dump
FR3128443A1 (fr) 2021-10-25 2023-04-28 Airbus Operations (S.A.S.) Ensemble de propulsion d’aéronef comprenant un échangeur thermique à plaques, de section longitudinale hexagonale, positionné dans une bifurcation

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US4971137A (en) * 1989-11-09 1990-11-20 American Energy Exchange, Inc. Air-to-air heat exchanger with frost preventing means
US5123242A (en) * 1990-07-30 1992-06-23 General Electric Company Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine
FR2734319B1 (fr) * 1995-05-15 1997-07-18 Aerospatiale Dispositif pour prelever et refroidir de l'air chaud au niveau d'un moteur d'aeronef
IL114613A (en) * 1995-07-16 1999-09-22 Tat Ind Ltd Parallel flow condenser heat exchanger
US5967461A (en) * 1997-07-02 1999-10-19 Mcdonnell Douglas Corp. High efficiency environmental control systems and methods
FR2839948B1 (fr) * 2002-05-22 2004-12-17 Airbus France Echangeur pour circuit de conditionnement d'air d'aeronef et ensemble de propulsion integrant un tel echangeur
US7607308B2 (en) * 2005-12-08 2009-10-27 General Electric Company Shrouded turbofan bleed duct
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US7856824B2 (en) * 2007-06-25 2010-12-28 Honeywell International Inc. Cooling systems for use on aircraft

Also Published As

Publication number Publication date
EP1907281B1 (fr) 2018-03-07
FR2889250B1 (fr) 2007-09-07
EP1907281A1 (fr) 2008-04-09
JP2009503332A (ja) 2009-01-29
CA2615273A1 (fr) 2007-02-01
US8522529B2 (en) 2013-09-03
US20090025366A1 (en) 2009-01-29
WO2007012722A1 (fr) 2007-02-01
JP4887364B2 (ja) 2012-02-29
FR2889250A1 (fr) 2007-02-02
CN101228069B (zh) 2012-06-06
BRPI0614447A2 (pt) 2011-03-29
CN101228069A (zh) 2008-07-23
CA2615273C (fr) 2015-06-02
RU2008107594A (ru) 2009-09-10

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Legal Events

Date Code Title Description
PC43 Official registration of the transfer of the exclusive right without contract for inventions

Effective date: 20120221

MM4A The patent is invalid due to non-payment of fees

Effective date: 20140708